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XTreme EFIS - MGL Avionics

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<strong>XTreme</strong> Operating Manual Page 6<br />

3.1 <strong>EFIS</strong> display<br />

The <strong>EFIS</strong> is displayed in a full screen format.<br />

3.1.1 Heading tape<br />

The heading tape is located at the top of the <strong>EFIS</strong> screen. The heading bug will be displayed in yellow if it is in the view<br />

area else it will turn cyan. The heading bug will always point to the shortest route to achieve the correct heading. The<br />

heading bug can be changed in the <strong>EFIS</strong>/MFD quick select menu. The heading is corrected for attitude while pitching and<br />

rolling (<strong>MGL</strong> <strong>Avionics</strong> AHRS unit required (SP4/SP5)).The Compass parameters can be configured in the “COMPASS<br />

SETUP” menu.<br />

3.1.2 Ground Speed<br />

This is located in the top left corner of the <strong>EFIS</strong> display. The ground speed value will only be displayed when a valid 2D or<br />

3D GPS fix has been achieved.<br />

3.1.3 Local Pressure Settings (QNH)<br />

This is located in the top right corner of the <strong>EFIS</strong> display. Turn the rotary control to change the local pressure setting. The<br />

local pressure can be displayed in mB or in “HG.<br />

3.1.4 True Airspeed (TAS)<br />

This is located in the bottom left corner of the <strong>EFIS</strong> display. TAS is used for most internal calculations where air distance<br />

is of importance.<br />

What is TAS and how is it calculated ?<br />

TAS is indicated airspeed (ASI) compensated for altitude and temperature. Often pilots ignore the effect of temperature<br />

and only take altitude into account when converting ASI to TAS. For practical purposes this is quite accurate and gives a<br />

good reflection on your true airspeed. Keeping in mind that ASI measurement is subject to errors caused by airflow<br />

around your aircraft, there seems little point in taking this calculation to absolute resolution.<br />

Again, we have decided to use a formula often used by pilots. This way the instrument reading will agree with what pilots<br />

are used to.<br />

Add 1.75% of IAS per 1000 ft (304.9 m) increase in altitude above sea level.<br />

We assume here that IAS = RAS (rectified air speed).

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